WO1987005369A1 - Propeller shaft for motor vehicle - Google Patents

Propeller shaft for motor vehicle Download PDF

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Publication number
WO1987005369A1
WO1987005369A1 PCT/GB1987/000154 GB8700154W WO8705369A1 WO 1987005369 A1 WO1987005369 A1 WO 1987005369A1 GB 8700154 W GB8700154 W GB 8700154W WO 8705369 A1 WO8705369 A1 WO 8705369A1
Authority
WO
WIPO (PCT)
Prior art keywords
shaft
portions
elements
interfitting
propeller shaft
Prior art date
Application number
PCT/GB1987/000154
Other languages
French (fr)
Inventor
Leslie George Fisher
Original Assignee
Brd Company Limited
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Brd Company Limited filed Critical Brd Company Limited
Priority to GB8816053A priority Critical patent/GB2208313B/en
Publication of WO1987005369A1 publication Critical patent/WO1987005369A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C3/00Shafts; Axles; Cranks; Eccentrics
    • F16C3/02Shafts; Axles
    • F16C3/03Shafts; Axles telescopic
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D3/00Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
    • F16D3/02Yielding couplings, i.e. with means permitting movement between the connected parts during the drive adapted to specific functions
    • F16D3/06Yielding couplings, i.e. with means permitting movement between the connected parts during the drive adapted to specific functions specially adapted to allow axial displacement

Definitions

  • This invention relates to a transmission shaft for use as the longitudinal shaft (usually, and herein, termed the propeller shaft) of a motor vehicle.
  • a transmission shaft for use as the longitudinal shaft (usually, and herein, termed the propeller shaft) of a motor vehicle.
  • Such a shaft is used for power transmission between a forwardly mounted engine unit and a rearwardly mounted differential gear unit, or gearbox and differential, in a vehicle.
  • a vehicle's propeller shaft it is usual to provide for a vehicle's propeller shaft to be capable of accommodating a relatively small change in the length of the shaft. Such a change in length is necessary to facilitate installation of the shaft and to accommodate geometrical changes with suspension movement and movement of the engine unit in service and may be provided by a sliding splined joint forming part of the shaft. If, however, the vehicle is involved in an accident involving front and/or rear impact, the shortening of the shaft length allowed for in its design may be exceeded as the body structure of the vehicle collapses longitudinally. It will be appreciated that it is usual to design the body structure of some vehicles, particular modern passenger cars, to absorb impact energy by progressive collapse of the front and rear parts thereof.
  • the propeller shaft will act as a rigid strut, which can buckle with possible dangerous consequences. For example, it may puncture the vehicle's fuel tank, cause damage to fuel lines, possibly enter the passenger compartment of the vehicle, or cause the engine unit to be displaced in an undesirable manner such as to enter the passenger compartment of the vehicle. Accordingly, it would be desirable if the propeller shaft were capable of axial collapse under such accident conditions, to avoid the above mentioned dangerous effects.
  • the shaft should, of course, perform as an ordinary shaft in normal service. Further, if the shaft were to be capable of collapsing progressively and absorbing energy in so doing, it could assist the energy absorbing design of the structure of the vehicle and increase overall vehicle safety. It is the object of the present invention to provide a propeller shaft which meets these requirements.
  • a propeller shaft including two tubular shaft elements having portions interfitting axially with one another and of a cross-sectional shape providing for transmission of torque therebetween and to prevent relative axial displacement between said elements under axial loads encountered in normal service, and wherein the configuration of said interfitting portions is such that, during shortening of the shaft by relative axial displacement between said shaft elements under excess axial load, at least one of said shaft elements is subject to progressive deformation thereby to absorb energy.
  • the requirement for energy absorbtion to enable the propeller shaft to partake in the energy absorbing deformation of the rest of the vehicle structure is met.
  • the simplest safety requirement would, of course, be met if the shaft collapsed without further resistance after the initial resistance to collapse is overcome, but then the shaft would take no further part in controlling the progressive deformation of the vehicle's structure.
  • a motor vehicle propeller shaft may rotate at a very high speed, e.g. several thousands of revolution per minute. It is important that the bending stiffness of such a shaft should be sufficient to ensure that the shaft remains straight and in balance at such speeds. Therefore the axially interfitting torque transmitting connection between the two tubular shaft elements must be of such a character as " to provide sufficient bending rigidity in the shaft.
  • said shaft elements adjacent said interfitting portions are of circular cross-sectional shape, and said interfitting portions thereof are deformed together to a splined configuration, i.e. one having circumferentially spaced axially extending projections and recesses.
  • the shaft element whose interfitting portion is innermost may be arranged to be progressively deformed during collapse of the shaft, by having its undeformed outside diameter greater than the minor diameter of the deformed portion of the outer shaft element. As will be described hereafter, the difference between such dimensions determines the force required to be exerted during shortening of the shaft.
  • the invention also provides a method of manufacturing the propeller shaft as above described, comprising assembling portions of two tubular shaft elements together in interfitting relation and deforming said portions together to provide a cross-sectional shape for torque transmission therebetween and a connection of a tightness sufficient to resist relative axial displacement between said elements under axial loads encountered in normal service, at least one of said deformed portions having a dimension arranged to cause progressive deformation of the other sha ' ft element during shortening of the shaft by relative axial displacement between said shaft elements under excess axial load.
  • Figure 1 is an elevation, partly in section, of part of a propeller shaft according to the invention
  • Figure 2 is a longitudinal cross-section, in two planes of Figure 3, of part of the shaft assembly illustrating manufacture thereof;
  • Figure 3 is a transverse cross-section through part of the shaft assembly.
  • FIG. 1 of the drawings there is shown part of a propeller shaft according to the invention.
  • a Hookes joint 10 of which one yoke is connected to a drive flange 11 and the other yoke is welded to a tubular shaft element 12.
  • the tubular shaft element 12 is connected at 13, by a torque transmitting connection as described hereafter, to a further tubular shaft element 14 which is itself welded to the outer element 15 of a slip spline joint whose inner element is indicated at 16.
  • the remainder of the shaft is not shown.
  • the spline joint 15, 16 provides for length adjustment of the shaft to facilitate installation and to accommodate relatively small shaft length changes in use.
  • tubular element 12 is of appreciably greater diameter than tubular element 14 and a portion 17 thereof is swaged down to a smaller diameter.
  • a portion 18 of tubular element 14 is expanded to a diameter such that portions 17, 18 closely telescopically interfit axially with one another.
  • Such interfitting portions are then deformed simultaneously with one another to a splined torque transmitting configuration having interfitting circumferentially spaced axially extending projections and recesses.
  • This deformation is effected by inserting a mandrel 19 into the portion 18 of shaft element 14, the mandrel having an external surface of the required configuration, and inwardly deforming circumferentially spaced parts 17a, 18a of the portions 17, 18 together.
  • This is effected by axial movement of a plurality of circumferentially spaced rollers as 20, in the direction of arrow 21, in engagement with the exterior of portion 17.
  • the extreme end 22 of portion 18 remains at its expanded dimension.
  • the dimensions of the shaft element 14, and roller 20 and mandrel 19, are selected so that the minor diameter of the deformed portion 17 of the outer tubular shaft element 12, indicated as A in Figure 3, is less than the outside diameter of the undeformed inner shaft element 14, the latter dimension being indicated as B in Figure 2.
  • the length of the interfitting and deformed portions 17, 18 must be sufficient to ensure torsional rigidity and bending stiffness in the complete shaft.

Abstract

A propeller shaft for a motor vehicle, incorporating two shaft elements (12, 14) including portions (17, 18) interfitting axially with one another and deformed to a torque transmitting cross-sectional shape, so that frictional forces therebetween are sufficient to prevent relative axial movement in normal service. Under accident conditions, however, the shaft is able to collapse axially during which one of the shaft elements (14) is progressively deformed by the other to provide progressive absorption of energy.

Description

PROPELLER SHAFT FOR MOTOR VEHICLE
This invention relates to a transmission shaft for use as the longitudinal shaft (usually, and herein, termed the propeller shaft) of a motor vehicle. Such a shaft is used for power transmission between a forwardly mounted engine unit and a rearwardly mounted differential gear unit, or gearbox and differential, in a vehicle.
It is usual to provide for a vehicle's propeller shaft to be capable of accommodating a relatively small change in the length of the shaft. Such a change in length is necessary to facilitate installation of the shaft and to accommodate geometrical changes with suspension movement and movement of the engine unit in service and may be provided by a sliding splined joint forming part of the shaft. If, however, the vehicle is involved in an accident involving front and/or rear impact, the shortening of the shaft length allowed for in its design may be exceeded as the body structure of the vehicle collapses longitudinally. It will be appreciated that it is usual to design the body structure of some vehicles, particular modern passenger cars, to absorb impact energy by progressive collapse of the front and rear parts thereof. Under these circumstances, the propeller shaft will act as a rigid strut, which can buckle with possible dangerous consequences. For example, it may puncture the vehicle's fuel tank, cause damage to fuel lines, possibly enter the passenger compartment of the vehicle, or cause the engine unit to be displaced in an undesirable manner such as to enter the passenger compartment of the vehicle. Accordingly, it would be desirable if the propeller shaft were capable of axial collapse under such accident conditions, to avoid the above mentioned dangerous effects. The shaft should, of course, perform as an ordinary shaft in normal service. Further, if the shaft were to be capable of collapsing progressively and absorbing energy in so doing, it could assist the energy absorbing design of the structure of the vehicle and increase overall vehicle safety. It is the object of the present invention to provide a propeller shaft which meets these requirements.
According to the invention, we provide a propeller shaft including two tubular shaft elements having portions interfitting axially with one another and of a cross-sectional shape providing for transmission of torque therebetween and to prevent relative axial displacement between said elements under axial loads encountered in normal service, and wherein the configuration of said interfitting portions is such that, during shortening of the shaft by relative axial displacement between said shaft elements under excess axial load, at least one of said shaft elements is subject to progressive deformation thereby to absorb energy.
By arranging at least one of the shaft elements progressively to be deformed by the other of the shaft elements as the shaft collapses axially, the requirement for energy absorbtion to enable the propeller shaft to partake in the energy absorbing deformation of the rest of the vehicle structure is met. The simplest safety requirement would, of course, be met if the shaft collapsed without further resistance after the initial resistance to collapse is overcome, but then the shaft would take no further part in controlling the progressive deformation of the vehicle's structure.
In use, a motor vehicle propeller shaft may rotate at a very high speed, e.g. several thousands of revolution per minute. It is important that the bending stiffness of such a shaft should be sufficient to ensure that the shaft remains straight and in balance at such speeds. Therefore the axially interfitting torque transmitting connection between the two tubular shaft elements must be of such a character as "to provide sufficient bending rigidity in the shaft.
Preferably said shaft elements adjacent said interfitting portions are of circular cross-sectional shape, and said interfitting portions thereof are deformed together to a splined configuration, i.e. one having circumferentially spaced axially extending projections and recesses.
By deforming said portions of the shaft elements together, a backlash free connection is established therebetween, which is rigid with respect to bending of the shaft.
The shaft element whose interfitting portion is innermost may be arranged to be progressively deformed during collapse of the shaft, by having its undeformed outside diameter greater than the minor diameter of the deformed portion of the outer shaft element. As will be described hereafter, the difference between such dimensions determines the force required to be exerted during shortening of the shaft. The invention also provides a method of manufacturing the propeller shaft as above described, comprising assembling portions of two tubular shaft elements together in interfitting relation and deforming said portions together to provide a cross-sectional shape for torque transmission therebetween and a connection of a tightness sufficient to resist relative axial displacement between said elements under axial loads encountered in normal service, at least one of said deformed portions having a dimension arranged to cause progressive deformation of the other sha'ft element during shortening of the shaft by relative axial displacement between said shaft elements under excess axial load.
The invention will now be described by way of example with reference to the accompanying drawings, of which:-
Figure 1 is an elevation, partly in section, of part of a propeller shaft according to the invention;
Figure 2 is a longitudinal cross-section, in two planes of Figure 3, of part of the shaft assembly illustrating manufacture thereof;
Figure 3 is a transverse cross-section through part of the shaft assembly.
Referring firstly to Figure 1 of the drawings, there is shown part of a propeller shaft according to the invention. At one end of the shaft, there is a Hookes joint 10 of which one yoke is connected to a drive flange 11 and the other yoke is welded to a tubular shaft element 12. The tubular shaft element 12 is connected at 13, by a torque transmitting connection as described hereafter, to a further tubular shaft element 14 which is itself welded to the outer element 15 of a slip spline joint whose inner element is indicated at 16. The remainder of the shaft is not shown. The spline joint 15, 16 provides for length adjustment of the shaft to facilitate installation and to accommodate relatively small shaft length changes in use.
Referring now to Figures 2 and 3 of the drawing, the torque transmitting connection 13 and the method of manufacture thereof are described in or'e detail.
Initially, tubular element 12 is of appreciably greater diameter than tubular element 14 and a portion 17 thereof is swaged down to a smaller diameter. A portion 18 of tubular element 14 is expanded to a diameter such that portions 17, 18 closely telescopically interfit axially with one another. Such interfitting portions are then deformed simultaneously with one another to a splined torque transmitting configuration having interfitting circumferentially spaced axially extending projections and recesses. This deformation is effected by inserting a mandrel 19 into the portion 18 of shaft element 14, the mandrel having an external surface of the required configuration, and inwardly deforming circumferentially spaced parts 17a, 18a of the portions 17, 18 together. This is effected by axial movement of a plurality of circumferentially spaced rollers as 20, in the direction of arrow 21, in engagement with the exterior of portion 17. The extreme end 22 of portion 18 remains at its expanded dimension.
The dimensions of the shaft element 14, and roller 20 and mandrel 19, are selected so that the minor diameter of the deformed portion 17 of the outer tubular shaft element 12, indicated as A in Figure 3, is less than the outside diameter of the undeformed inner shaft element 14, the latter dimension being indicated as B in Figure 2.
The length of the interfitting and deformed portions 17, 18 must be sufficient to ensure torsional rigidity and bending stiffness in the complete shaft.
In use of the shaft, frictional forces between portions 17, 18 as a result of the deformation thereof, together with the axial interfitting pro'vided by the minor diameter of portion 17 being less than dimension B and less than the diameter of the extreme end 22 of portion 18, are sufficient to prevent any relative movement between the shaft elements 12, 14 under axial forces which normally arise. In the event of an accident sufficiently severe to attempt to cause shortening of the propeller shaft beyond that able to be accommodated by the splined joint 15, 16, this is likely to apply a sufficient axial force to the shaft to overcome friction between portions 17, 18 and cause the shaft to collapse axially. During such axial collapse, the fact that dimension A is less than dimension B means that the shaft element 14 will be deformed by portions 17 of shaft element 12 as the shaft shortens. The shaft thus progressively absorbs energy during its axial collapse to enhance safety as above described. The difference between dimensions A and B determines the magnitude of such energy absorbtion.
Although one torque transmitting configuration to which the shaft elements 12, 14 are deformed has been described, it will be appreciated that other torque transmitting configurations could be adopted. Further, although as above described it is the shaft element 14 which is progressively deformed to absorb energy during axial collapse of the shaft, in a shaft of suitable configuration the other, or possibly both, of the shaft elements may provide for such energy absorbtion.

Claims

1. A propeller shaft including two tubular shaft elements (12, 14) having portions (17, 18) interfitting axially with one another and of a cross-sectional shape providing for transmission of torque therebetween and to prevent relative axial displacement between said elements (12, 14) under axial loads encountered in normal service, and wherein the configuration of said interfitting portions (17, 18) is such that, during shortening of the shaft by relative axial displacement between said shaft elements under excess axial load, at least one of said shaft elements (14) is subject to' progressive deformation thereby to absorb energy.
2. A propeller shaft according to Claim 1 wherein said shaft elements (12, 14) adjacent said interfitting portions are of circular cross-sectional shape, and said interfitting portions (17, 18) thereof have circumferentially spaced axially extending projections and recesses.
3. A propeller shaft according to Claim 2 wherein circumferentially spaced parts (17a, 18a) of said portions (17, 18) have been deformed together to said cross-sectional shape.
4. A propeller shaft according to Claim 3 wherein the minor diameter (A) of each said deformed parts (17a) of the outer shaft element (12) is less than the outside diameter (B) of the undeformed portion of said inner shaft element (14) .
5. A method of manufacturing a propeller shaft including assembling portions (17, 18) of two tubular shaft elements (12, 14) together in interfitting relation and deforming said portions (17, 18) together to provide a cross-sectional shape for torque transmission therebetween and a connection of a tightness sufficient to resist relative axial displacement between said elements under axial loads encountered in normal service, at least one of said deformed portions (17) having a dimension arranged to cause progressive deformation of the other shaft element (14) during shortening of the shaft by relative axial displacement between said shaft elements under excess axial load.
6. A method according to Claim 5 wherein said deformation comprises inwardly displacing a number of circumferentially spaced axially extending parts (17a, 18a) of said portions (17, 18) .
7. A method according to Claim 6 wherein said displacement of each of said parts is effected by a roller (20).
8. A method according to Claim 6 or Claim 7, further comprising supporting said portions (17, 18) by an internal mandrel (19) during said deformation.
PCT/GB1987/000154 1986-03-08 1987-03-05 Propeller shaft for motor vehicle WO1987005369A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8816053A GB2208313B (en) 1986-03-08 1987-03-05 Propeller shaft for motor vehicle

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB868605769A GB8605769D0 (en) 1986-03-08 1986-03-08 Propeller shaft for motor vehicle
GB8605769 1986-03-08

Publications (1)

Publication Number Publication Date
WO1987005369A1 true WO1987005369A1 (en) 1987-09-11

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ID=10594278

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/GB1987/000154 WO1987005369A1 (en) 1986-03-08 1987-03-05 Propeller shaft for motor vehicle

Country Status (5)

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EP (1) EP0298079A1 (en)
JP (1) JPH01502442A (en)
CA (1) CA1286119C (en)
GB (2) GB8605769D0 (en)
WO (1) WO1987005369A1 (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2650036A1 (en) * 1989-06-24 1991-01-25 Gkn Automotive Ag CONNECTING SLEEVE ASSEMBLY DEVICE FOR TUBULAR SHAFT
FR2663696A1 (en) * 1990-06-23 1991-12-27 Gkn Automotive Ag DRIVE SHAFT OF A MOTOR VEHICLE, IN PARTICULAR LONGITUDINAL SHAFT, ABSORBING ENERGY IN THE EVENT OF A VEHICLE COLLISION.
DE4113709A1 (en) * 1991-04-26 1992-10-29 Audi Ag Tubular drive shaft - has sleeve enveloping resilient element, has wider section covering latter, and counteracts collapse of shaft during deformation
DE4309622A1 (en) * 1993-03-24 1994-09-29 Daimler Benz Ag Propeller shaft for the drive line of a motor vehicle
DE4343470C1 (en) * 1993-12-20 1995-02-23 Gkn Automotive Ag Split longitudinal shaft in the driveline of a motor vehicle
DE19515180A1 (en) * 1995-04-25 1996-11-07 Bayerische Motoren Werke Ag Articulated shaft for torque transfer and energy absorption in vehicle
GB2337098A (en) * 1998-05-07 1999-11-10 Gen Electric Axially and rotationally adjustable drive shaft assembly
GB2371614A (en) * 2001-01-26 2002-07-31 Dana Corp Method of manufacturing an axially collapsible driveshaft
EP1698787A3 (en) * 2005-03-05 2008-07-30 Dana Corporation Method of manufacturing an axially collapsible splined assembly
WO2012044906A2 (en) * 2010-09-30 2012-04-05 Hendrickson Usa, L.L.C. Brake system component axle mount
US8454040B2 (en) 2010-09-30 2013-06-04 Hendrickson Usa, L.L.C. Heavy-duty axle-to-beam connection
CN110621899A (en) * 2017-04-25 2019-12-27 Gkn 动力传动系统有限公司 Shaft connection and drive shaft having such a shaft connection
US10948008B2 (en) 2014-10-17 2021-03-16 Thyssenkrupp Presta Ag Steering shaft and method for producing a profiled hollow shaft for a telescopic steering shaft of a motor vehicle
US11518190B2 (en) 2017-10-23 2022-12-06 Hendrickson United Kingdom Ltd Heavy-duty connections e.g. for axle/suspension systems

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6368225B1 (en) 1999-12-30 2002-04-09 Spicer Driveshaft, Inc. Axially collapsible driveshaft assembly and method of manufacturing same

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1331015A (en) * 1962-08-03 1963-06-28 tubular transmission element with axial splines and method of making the same
US3394612A (en) * 1966-09-15 1968-07-30 Gen Motors Corp Steering column assembly
FR2078950A5 (en) * 1970-02-23 1971-11-05 Gen Motors Holdens
FR2508860A1 (en) * 1981-07-03 1983-01-07 Supervis Ets STEERING AXIS FOR STEERING DEVICE FOR MOTOR VEHICLES
DE3241715A1 (en) * 1982-11-11 1984-05-24 Gelenkwellenbau Gmbh, 4300 Essen Telescopic shaft

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1331015A (en) * 1962-08-03 1963-06-28 tubular transmission element with axial splines and method of making the same
US3394612A (en) * 1966-09-15 1968-07-30 Gen Motors Corp Steering column assembly
FR2078950A5 (en) * 1970-02-23 1971-11-05 Gen Motors Holdens
FR2508860A1 (en) * 1981-07-03 1983-01-07 Supervis Ets STEERING AXIS FOR STEERING DEVICE FOR MOTOR VEHICLES
DE3241715A1 (en) * 1982-11-11 1984-05-24 Gelenkwellenbau Gmbh, 4300 Essen Telescopic shaft

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2650036A1 (en) * 1989-06-24 1991-01-25 Gkn Automotive Ag CONNECTING SLEEVE ASSEMBLY DEVICE FOR TUBULAR SHAFT
GB2233425B (en) * 1989-06-24 1992-04-01 Gkn Automotive Ag A connecting assembly
FR2663696A1 (en) * 1990-06-23 1991-12-27 Gkn Automotive Ag DRIVE SHAFT OF A MOTOR VEHICLE, IN PARTICULAR LONGITUDINAL SHAFT, ABSORBING ENERGY IN THE EVENT OF A VEHICLE COLLISION.
DE4119359A1 (en) * 1990-06-23 1992-01-09 Gkn Automotive Ag Fibre-bonded tubular shaft - deforms when vehicle crashes and has energy absorbing characteristics matching bodywork
GB2245954A (en) * 1990-06-23 1992-01-15 Gkn Automotive Ag Motor vehicle propeller shaft
GB2245954B (en) * 1990-06-23 1994-09-28 Gkn Automotive Ag Motor vehicle propeller shaft
DE4113709A1 (en) * 1991-04-26 1992-10-29 Audi Ag Tubular drive shaft - has sleeve enveloping resilient element, has wider section covering latter, and counteracts collapse of shaft during deformation
DE4309622A1 (en) * 1993-03-24 1994-09-29 Daimler Benz Ag Propeller shaft for the drive line of a motor vehicle
DE4309622C2 (en) * 1993-03-24 1995-08-17 Daimler Benz Ag PTO shaft for the drive train of a motor vehicle
DE4343470C1 (en) * 1993-12-20 1995-02-23 Gkn Automotive Ag Split longitudinal shaft in the driveline of a motor vehicle
DE19515180A1 (en) * 1995-04-25 1996-11-07 Bayerische Motoren Werke Ag Articulated shaft for torque transfer and energy absorption in vehicle
US6083108A (en) * 1998-05-07 2000-07-04 General Electric Co. Collapsible and relatively rotatable drive shaft
GB2337098A (en) * 1998-05-07 1999-11-10 Gen Electric Axially and rotationally adjustable drive shaft assembly
GB2337098B (en) * 1998-05-07 2003-04-09 Gen Electric Collapsible and relatively rotatable drive shaft
GB2371614A (en) * 2001-01-26 2002-07-31 Dana Corp Method of manufacturing an axially collapsible driveshaft
GB2371614B (en) * 2001-01-26 2004-08-18 Dana Corp Method of manufacturing an axially collapsible driveshaft assembly
EP1698787A3 (en) * 2005-03-05 2008-07-30 Dana Corporation Method of manufacturing an axially collapsible splined assembly
WO2012044906A3 (en) * 2010-09-30 2012-07-05 Hendrickson Usa, L.L.C. Brake system component axle mount
WO2012044906A2 (en) * 2010-09-30 2012-04-05 Hendrickson Usa, L.L.C. Brake system component axle mount
US8454040B2 (en) 2010-09-30 2013-06-04 Hendrickson Usa, L.L.C. Heavy-duty axle-to-beam connection
AU2011308673B2 (en) * 2010-09-30 2014-11-20 Hendrickson Usa, L.L.C. Brake system component axle mount
US10953499B2 (en) 2010-09-30 2021-03-23 Hendrickson Usa, L.L.C. Brake system component axle mount
US10948008B2 (en) 2014-10-17 2021-03-16 Thyssenkrupp Presta Ag Steering shaft and method for producing a profiled hollow shaft for a telescopic steering shaft of a motor vehicle
CN110621899A (en) * 2017-04-25 2019-12-27 Gkn 动力传动系统有限公司 Shaft connection and drive shaft having such a shaft connection
US11384797B2 (en) 2017-04-25 2022-07-12 Gkn Driveline Deutschland Gmbh Drive shaft connection
CN110621899B (en) * 2017-04-25 2023-03-10 Gkn 动力传动系统有限公司 Shaft connection and drive shaft having such a shaft connection
US11518190B2 (en) 2017-10-23 2022-12-06 Hendrickson United Kingdom Ltd Heavy-duty connections e.g. for axle/suspension systems

Also Published As

Publication number Publication date
GB2208313A (en) 1989-03-22
GB8605769D0 (en) 1986-04-16
EP0298079A1 (en) 1989-01-11
CA1286119C (en) 1991-07-16
GB2208313B (en) 1989-11-08
JPH01502442A (en) 1989-08-24
GB8816053D0 (en) 1988-09-21

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